Buckling Analysis using Femap w/ Nastran Advanced Nonlinear
Buckling Analysis using Femap w/ Nastran Advanced Nonlinear
What is in this webinar?
In this webinar, Alex Skavdahl will explore post-buckled behavior by running a model far in excess of when it buckles. The advanced non-linear solver can track the post-buckled behavior well into the plastic range. It’s perfect for light aerospace structures where skins are designed to buckle before limit load. The first demonstration will be on a thin-walled cylinder and the second demonstration will be on a box beam structure.
What is in this webinar? Siemens Principle Applications Engineer Chip Fricke will be presenting this webinar on Simcenter Nastran Solutions 401 & 402. Some of the topics covered will be: Overview of Simcenter Nastran Multi-step Nonlinear Solutions ...
What is in this webinar? This webinar shows a live demonstration of applying loads and constraints to a meshed finite element model (FEM) in Femap, and running a Normal Modes and Static Analyses in the NX Nastran solver.
Inertia Relief balances out the applied loads with equal and opposite accelerations, creating a state of static equilibrium and eliminating the need for constraints. Nick covers the topic of Inertial Relief in Femap w/ NX Nastran, including: What is ...
What is in this webinar? Static Aeroelastic Trim Analysis The first topic to be covered will be how to set up an aeroelastic trim analysis on an entire aircraft, and how to interpret the results. This will include how to setup a control surface, ...